CN207536134U - A kind of anti-dismounting device being integrated in unmanned plane locator - Google Patents
A kind of anti-dismounting device being integrated in unmanned plane locator Download PDFInfo
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- CN207536134U CN207536134U CN201721533032.3U CN201721533032U CN207536134U CN 207536134 U CN207536134 U CN 207536134U CN 201721533032 U CN201721533032 U CN 201721533032U CN 207536134 U CN207536134 U CN 207536134U
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- China
- Prior art keywords
- locator
- unmanned plane
- conductive sheet
- unit
- dismounting
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Abstract
The utility model is related to unmanned plane positioning device fields, disclose a kind of anti-dismounting device being integrated in unmanned plane locator.It is created by the utility model, after to integrating the anti-unmanned plane locator progress effectively installation for removing device, it may be constructed the screw by passing through screw installing hole, the anti-dismounting measure loop that two conductive sheets and break detection circuit unit are formed, and then it can reflect whether unmanned plane locator is removed extremely according to the anti-breaking testing result for removing measure loop, and when finding to be removed extremely, can the abnormal dismounting information and current location information of in-time generatin be automatically uploaded to supervision center using the existing capability unit of unmanned plane locator, so that backstage is reminded to take corresponding measure to affiliated unmanned plane in time, backstage is prevented by dummy location information deception, effectively ensure supervision effect.In addition, the anti-dismounting device also has many advantages, such as dismounting accuracy of judgement, simple in structure, at low cost and be easily achieved, conducive to practical promotion and application.
Description
Technical field
The utility model is related to unmanned plane positioning device fields, and in particular, to one kind is integrated in unmanned plane locator
Anti- dismounting device.
Background technology
With the fast development of unmanned plane industry, unmanned plane is accurately positioned the key one for already becoming industry development
Ring has important practical significance for the supervision of unmanned plane.Currently the working method of unmanned plane locator is：On in real time
The current location information of unmanned plane is reported to supervision center, and supervise using the automation that background program is implemented to unmanned plane.But
For current unmanned plane locator, if it is artificially deliberately removed, it will cause background program that can not get really
Unmanned plane location information, so as to lose effective supervision to unmanned plane.
Utility model content
It can lead to the problem of supervision loophole, the utility model occur after being removed for aforementioned existing unmanned plane locator
Provide a kind of anti-dismounting device being integrated in unmanned plane locator.
The technical solution adopted in the utility model provides a kind of anti-dismounting device being integrated in unmanned plane locator,
Including locator processing unit, locator satellite positioning unit, locator Transmit-Receive Unit, locator storage unit, burn out detection
Circuit unit and insulated mounting plate, wherein, the locator processing unit communicates to connect the locator satellite positioning list respectively
First, described locator Transmit-Receive Unit and the locator storage unit；
The detection signal output end of the break detection circuit unit is electrically connected the first conductive sheet, the break detection circuit
The detection signal reflux end of unit is electrically connected the second conductive sheet, and the testing result output terminal of the break detection circuit unit is electrically connected
The input terminal of the locator processing unit is connect, wherein, first conductive sheet and the second conductive sheet compartment of terrain are embedded in institute
It states in insulated mounting plate；
Several screw installing holes are offered on the insulated mounting plate, and a wherein screw installing hole is made to extend through institute
State the first conductive sheet and second conductive sheet.
Optimization, the break detection circuit unit includes DC power supply, first resistor and second resistance；The direct current
Electrical series, the detection signal reflux end are electrically connected successively for source, the first resistor and the detection signal output end
One end of the second resistance and the testing result output terminal, the other end ground connection of the second resistance.
It advanced optimizes, the break detection circuit unit further includes diode and electrolytic capacitor；The detection signal
Reflux end is also electrically connected the anode of the diode, and the cathode of the diode is electrically connected the anode of the electrolytic capacitor, described
The cathode ground connection of electrolytic capacitor；The anode of the electrolytic capacitor as feeder ear be electrically connected the locator processing unit,
The power end of the locator satellite positioning unit, the locator Transmit-Receive Unit and the locator storage unit.
Optimization, the insulated mounting plate is not less than the PCB substrate of 5mm for thickness.
It advanced optimizes, first conductive sheet or second conductive sheet are copper coin of the thickness not less than 1mm.
It advanced optimizes, first conductive sheet is set with second sheet parallel, and makes the distance of the two not
Less than 2mm.
Optimization, the locator satellite positioning unit using model UM220-III the Big Dipper/GPS dual systems are wireless
Locating module.
To sum up, using the anti-dismounting device provided by the utility model being integrated in unmanned plane locator, have as follows
Advantageous effect：(1) it after to integrating the anti-unmanned plane locator progress effectively installation for removing device, may be constructed by passing through spiral shell
The anti-dismounting measure loop that screw, two conductive sheets and the break detection circuit unit of silk mounting hole are formed, and then can be anti-according to this
The breaking testing result of measure loop is removed to reflect whether unmanned plane locator is removed extremely, and is finding to be removed extremely
When, can the abnormal of in-time generatin automatically be removed into information and current location using the existing capability unit of unmanned plane locator
Information is uploaded to supervision center, so that backstage is reminded to take corresponding measure to affiliated unmanned plane in time, prevents backstage by false position
Information deception is put, effectively ensures supervision effect；(2) unmanned plane locator can also be supplied using anti-dismounting measure loop
Electricity, so as to loop open circuit and send it is last report information (including abnormal dismounting information and current location information) after, automatically
It is stopped, can avoid continuing dummy location information to be sent to supervision center, be further conducive to ensure supervision effect；(3) institute
Stating anti-dismounting device also has many advantages, such as to remove accuracy of judgement, simple in structure, at low cost and be easily achieved, conducive to it is practical promote with
Using.
Description of the drawings
It in order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor
Under, it can also be obtained according to these attached drawings other attached drawings.
Fig. 1 is the anti-structure diagram for removing device provided by the utility model.
In above-mentioned attached drawing：1st, insulated mounting plate 101, screw installing hole 201, the first conductive sheet 202, the second conductive sheet.
Specific embodiment
Hereinafter reference will be made to the drawings, and describing the unmanned plane provided by the utility model that is integrated in detail by way of example determines
Anti- dismounting device in the device of position.It should be noted that the explanation of these way of example is used to help understand this reality
With novel, but the restriction to the utility model is not formed.
The terms "and/or", only a kind of incidence relation for describing affiliated partner, expression may have three kinds of passes
System, for example, A and/or B, can represent：Individualism A, individualism B exist simultaneously tri- kinds of situations of A and B, the terms
"/and " it is another affiliated partner relationship of description, expression may have two kinds of relationships, for example, A/ and B, can represent：Individually deposit
In A, two kinds of situations of individualism A and B, in addition, character "/" herein, it is that a kind of "or" is closed to typically represent forward-backward correlation object
System.
Embodiment one
Fig. 1 shows the anti-structure diagram for removing device provided by the utility model.The collection provided in this embodiment
Into the anti-dismounting device in unmanned plane locator, received including locator processing unit, locator satellite positioning unit, locator
Bill member, locator storage unit, break detection circuit unit and insulated mounting plate 1, wherein, the locator processing unit point
The locator satellite positioning unit, the locator Transmit-Receive Unit and the locator storage unit are not communicated to connect；It is described
The detection signal output end CSout of break detection circuit unit is electrically connected the first conductive sheet 201, the break detection circuit unit
Detection signal reflux end CSin be electrically connected the second conductive sheet 202, the testing result output terminal of the break detection circuit unit
CK is electrically connected the input terminal Vin of the locator processing unit, wherein, first conductive sheet 201 and second conductive sheet
202 compartment of terrain are embedded in the insulated mounting plate 1；Several screw installing holes 101 are offered on the insulated mounting plate 1, and
A wherein screw installing hole 101 is made to extend through first conductive sheet 201 and second conductive sheet 202.
As shown in Figure 1, in the anti-structure for removing device, the locator processing unit, the locator satellite
Positioning unit, the locator Transmit-Receive Unit and the locator storage unit are that the standard configuration of current unmanned plane locator is set
It is standby.Wherein, the locator processing unit is additionally operable to root in addition to the essential information processing function for being used to implement unmanned plane locator
According to the testing result from the break detection circuit unit, when finding that unmanned plane locator is removed extremely, automatically give birth to
Information is removed, and by the locator Transmit-Receive Unit by the abnormal dismounting information and from the locator satellite into abnormal
The current location information of positioning unit is uploaded to supervision center；The locator satellite positioning unit is used to carry out with position location satellite
Wireless communication obtains location information, preferably uses the dual mode satellite position receiver mould of model OBT2217BD/GPS in real time
Block, you can led using Beidou satellite navigation system or GPS (GlobalPositioningSystem, global positioning system) satellite
Boat system is positioned and navigational communications；The locator Transmit-Receive Unit is used to implement the wireless communication with supervision center, can
With but be not limited to using GPRS (GeneralPacketRadioService, general packet radio service technology) wireless receiving and dispatching mould
Block；The locator storage unit including but not limited to runs program, current operation mode information for storing various information
(such as factory mode or use pattern) and historical position information etc..
The break detection circuit unit is used in the detection signal output end CSout export detection signal, and in institute
It states detection signal reflux end CSin and receives the detection signal returned, to be judged between both ends according to reception result
Branch is conducting or open circuit, and exports corresponding testing result in the testing result output terminal CK.The insulated mounting plate 1
For providing the installation position of unmanned plane locator, so as to using the screw across the screw installing hole 101 by the unmanned plane
Locator is fixed on unmanned plane.It is designed simultaneously by aforementioned structure, (it is necessarily metallic screw to screw, has when mounted
Certain electric conductivity) it will necessarily be threadedly coupled respectively with first conductive sheet 201 and second conductive sheet 202, Jin Erke
Make the detection signal output end CSout and the detection signal reflux end CSin electrical communications using the conduction of screw.Thus
After to integrating the anti-unmanned plane locator progress effectively installation for removing device, the spiral shell by passing through screw installing hole may be constructed
The anti-dismounting measure loop that nail, two conductive sheets and break detection circuit unit are formed, and then can be according to the anti-dismounting measure loop
Breaking testing result reflect whether unmanned plane locator is removed extremely, and when finding to be removed extremely, can be automatically
The abnormal dismounting information and current location information of in-time generatin are uploaded to using the existing capability unit of unmanned plane locator
Supervision center so that backstage is reminded to take corresponding measure to affiliated unmanned plane in time, prevents backstage by dummy location information deception,
Effectively ensure supervision effect.
Optimization, the break detection circuit unit includes DC power supply VCC, first resistor R1 and second resistance R2；Institute
State DC power supply VCC, the first resistor R1 and the detection signal output end CSout electrical series successively, the detection letter
Number reflux end CSin be electrically connected one end of the second resistance R2 and the testing result output terminal CK, the second resistance
The other end ground connection of R2.As shown in Figure 1, the first resistor R1 is used for current limliting, the second resistance R2 for dividing, so as to
When anti-dismounting measure loop is not breaking, testing result output terminal CK output high level is made (to reflect the detection of normal mounting
As a result).And in anti-dismounting measure loop open circuit, the testing result output terminal CK will export low level, and (i.e. reflection is abnormal
The testing result of dismounting), so can burn out detection result accurately be fed back into the locator processing unit.
It advanced optimizes, the break detection circuit unit further includes diode D1 and electrolytic capacitor C1；The detection
Signal reflux end CSin is also electrically connected the anode of the diode D1, and the cathode of the diode D1 is electrically connected the electrolytic capacitor
The anode of C1, the cathode ground connection of the electrolytic capacitor C1；The anode of the electrolytic capacitor C1 is electrically connected as feeder ear VDD
The locator processing unit, the locator satellite positioning unit, the locator Transmit-Receive Unit and locator storage
The power end of unit.As shown in Figure 1, the electrolytic capacitor C1 is used to store electric energy, so as in anti-dismounting measure loop open circuit
Temporary source can be provided for other units, it is ensured that information can be reported (to remove information and present bit including abnormal last
Confidence ceases) it is uploaded to supervision center.The diode D1 is used to ensure the one-way of electric current, makes the testing result output terminal CK
Low level can be effectively exported in anti-dismounting measure loop open circuit.Thus anti-dismounting measure loop can also be utilized to unmanned plane
Locator is powered, so as to loop open circuit and send it is last report information after, be automatically stopped work, can avoid will be false
Location information continues to be sent to supervision center, is further conducive to ensure supervision effect.
Optimization, the insulated mounting plate 1 is not less than PCB (PrintedCircuit Board, the printing of 5mm for thickness
Circuit board) substrate.The insulating laminated plate that the PCB substrate is made of high molecular synthetic resin and reinforcing material is set by aforementioned
Meter can make insulated mounting plate 1 not only have suitable installation hardness, but also have preferable insulation effect, meet application demand.
It advanced optimizes, first conductive sheet 201 or second conductive sheet 202 are copper of the thickness not less than 1mm
Plate.Pass through previous designs, it can be ensured that screw across after the screw installing hole 101, can respectively with the described first conduction
Piece 201 or second conductive sheet 202 carry out effective in electrical contact, avoid the occurrence of erroneous judgement.
Both it advanced optimizing, first conductive sheet 201 is arranged in parallel with second conductive sheet 202, and make
Distance is not less than 2mm.Pass through aforementioned definition, it can be ensured that first conductive sheet 201 is effective with second conductive sheet 202
It electrically isolates, avoids the two direct short-circuit.
The anti-dismounting device being integrated in unmanned plane locator provided in this embodiment, has the advantages that：
(1) it after to integrating the anti-unmanned plane locator progress effectively installation for removing device, may be constructed by passing through screw installing hole
Screw, the anti-dismounting measure loop that forms of two conductive sheets and break detection circuit unit, and then can be detected according to anti-remove
The breaking testing result in circuit reflects whether unmanned plane locator is removed extremely, and when finding to be removed extremely, can from
The abnormal of in-time generatin is removed on information and current location information using the existing capability unit of unmanned plane locator dynamicly
Supervision center is reached, so that backstage is reminded to take corresponding measure to affiliated unmanned plane in time, prevents backstage by dummy location information
Deception, effectively ensures supervision effect；(2) anti-dismounting measure loop can also be utilized to be powered unmanned plane locator, so as to
Loop open circuit and send it is last report information (including abnormal dismounting information and current location information) after, be automatically stopped work
Make, can avoid continuing dummy location information to be sent to supervision center, be further conducive to ensure supervision effect；(3) tamper
Except device also has many advantages, such as to remove accuracy of judgement, simple in structure, at low cost and be easily achieved, conducive to practical promotion and application.
As described above, it can preferably realize the utility model.For a person skilled in the art, it is new according to this practicality
The labor that various forms of anti-dismounting devices being integrated in unmanned plane locator do not need to be creative is designed in the introduction of type
It is dynamic.These embodiments are changed in the case of the principle and spirit for not departing from the utility model, change, replace, are integrated
It is still fallen in the scope of protection of the utility model with modification.
Claims (7)
1. a kind of anti-dismounting device being integrated in unmanned plane locator, which is characterized in that including locator processing unit, positioning
Device satellite positioning unit, locator Transmit-Receive Unit, locator storage unit, break detection circuit unit and insulated mounting plate (1),
Wherein, the locator processing unit communicates to connect the locator satellite positioning unit, the locator Transmit-Receive Unit respectively
With the locator storage unit；
The detection signal output end (CSout) of the break detection circuit unit is electrically connected the first conductive sheet (201), the broken string
Detection signal reflux end (CSin) of detection circuit unit is electrically connected the second conductive sheet (202), the break detection circuit unit
Testing result output terminal (CK) be electrically connected the input terminal (Vin) of the locator processing unit, wherein, first conductive sheet
(201) and second conductive sheet (202) compartment of terrain is in the insulated mounting plate (1)；
Several screw installing holes (101) are offered on the insulated mounting plate (1), and make a wherein screw installing hole (101)
Extend through first conductive sheet (201) and second conductive sheet (202).
2. a kind of anti-dismounting device being integrated in unmanned plane locator as described in claim 1, which is characterized in that described disconnected
Line detection circuit unit includes DC power supply (VCC), first resistor (R1) and second resistance (R2)；
The DC power supply (VCC), the first resistor (R1) and the detection signal output end (CSout) are electrically gone here and there successively
Connection, detection signal reflux end (CSin) are electrically connected one end of the second resistance (R2) and testing result output
It holds (CK), the other end ground connection of the second resistance (R2).
3. a kind of anti-dismounting device being integrated in unmanned plane locator as claimed in claim 2, which is characterized in that described disconnected
Line detection circuit unit further includes diode (D1) and electrolytic capacitor (C1)；
Detection signal reflux end (CSin) is also electrically connected the anode of the diode (D1), the cathode of the diode (D1)
It is electrically connected the anode of the electrolytic capacitor (C1), the cathode ground connection of the electrolytic capacitor (C1)；
The anode of the electrolytic capacitor (C1) is electrically connected the locator processing unit, described fixed as feeder ear (VDD)
The power end of position device satellite positioning unit, the locator Transmit-Receive Unit and the locator storage unit.
4. a kind of anti-dismounting device being integrated in unmanned plane locator as described in claim 1, which is characterized in that described exhausted
Edge installing plate (1) is not less than the PCB substrate of 5mm for thickness.
5. a kind of anti-dismounting device being integrated in unmanned plane locator as claimed in claim 4, which is characterized in that described the
One conductive sheet (201) or second conductive sheet (202) are not less than the copper coin of 1mm for thickness.
6. a kind of anti-dismounting device being integrated in unmanned plane locator as claimed in claim 4, which is characterized in that described the
One conductive sheet (201) is arranged in parallel with second conductive sheet (202), and the distance of the two is made to be not less than 2mm.
7. a kind of anti-dismounting device being integrated in unmanned plane locator as described in claim 1, which is characterized in that described fixed
Position device satellite positioning unit uses the Big Dipper/GPS dual system wireless locating modules of model UM220-III.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721533032.3U CN207536134U (en) | 2017-11-16 | 2017-11-16 | A kind of anti-dismounting device being integrated in unmanned plane locator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721533032.3U CN207536134U (en) | 2017-11-16 | 2017-11-16 | A kind of anti-dismounting device being integrated in unmanned plane locator |
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| Publication Number | Publication Date |
|---|---|
| CN207536134U true CN207536134U (en) | 2018-06-26 |
Family
ID=62613815
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721533032.3U Expired - Fee Related CN207536134U (en) | 2017-11-16 | 2017-11-16 | A kind of anti-dismounting device being integrated in unmanned plane locator |
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| Country | Link |
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| CN (1) | CN207536134U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109521346A (en) * | 2019-01-14 | 2019-03-26 | 深圳市麦崇迪威科技有限公司 | Contact detection structure and detection mode of the wiring board voltage-withstand test to more PIN needles |
| CN116150820A (en) * | 2023-04-20 | 2023-05-23 | 粤港澳大湾区数字经济研究院(福田) | Aircraft management method based on confidential calculation coprocessor and aircraft |
-
2017
- 2017-11-16 CN CN201721533032.3U patent/CN207536134U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109521346A (en) * | 2019-01-14 | 2019-03-26 | 深圳市麦崇迪威科技有限公司 | Contact detection structure and detection mode of the wiring board voltage-withstand test to more PIN needles |
| CN116150820A (en) * | 2023-04-20 | 2023-05-23 | 粤港澳大湾区数字经济研究院(福田) | Aircraft management method based on confidential calculation coprocessor and aircraft |
| CN116150820B (en) * | 2023-04-20 | 2023-11-24 | 粤港澳大湾区数字经济研究院(福田) | Aircraft management method based on confidential calculation coprocessor and aircraft |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No. 31, Huaxin Road, Shunqing District, Nanchong, Sichuan Province Patentee after: Sichuan Yuyun Innovation Technology Co., Ltd. Address before: No. 31, Huaxin Road, Shunqing District, Nanchong, Sichuan Province Patentee before: NANCHONG YUYUN INNOVATION TECHNOLOGY Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180626 Termination date: 20201116 |
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| CF01 | Termination of patent right due to non-payment of annual fee |